H01Q1/288

Bi-Directional Flat Plate Foldable Unit and Bi-Directional Flat Plate Foldable Antenna Mechanism

The present invention discloses a bi-directional flat plate foldable unit, including a first row of antenna plates and a second row of antenna plates distributed along a first direction; the first row of antenna plates and the second row of antenna plates both include three antenna plates distributed in a second direction perpendicular to the first direction, three antenna plates in the first row of antenna plates and three antenna plates in the second row of antenna plates are set opposite to each other and hinged to form a first rotating pair; any two antenna plates adjacent to each other in the same row of antenna plates are hinged to form a second rotating pair; three antenna plates in the first row of antenna plates and three antenna plates in the second row of antenna plates are connected by a vertical support mechanism, and the first row of antenna plates are connected to the second row of antenna plates by a lateral support mechanism. The bi-directional flat plate foldable antenna mechanism includes at least two bi-directional flat plate foldable units mentioned above. The present invention facilitates the folding and unfolding of planar antennas with larger physical diameter and high rigidity.

Substrate-type antenna for global navigation satellite system

Provided is an antenna for receiving radio waves including frequencies in the L6 band unique to QZSS to realize accurate positioning by QZSS. A substrate-type antenna 1 comprises an arcuate antenna element 20 including a long arcuate antenna element 22 and a short arcuate antenna element 24, each of which includes an integral antenna element compatible with three frequency bands and a single antenna element compatible with one frequency band and arranged with a space from the integral antenna element. Each of the integral antenna element and the single antenna element extends from an outer peripheral part of the arcuate antenna element toward an inner peripheral part thereof. The substrate-type antenna 1 further comprises a plurality of connection units 34 connected to the long arcuate antenna element 22 and the short arcuate antenna element 24, respectively, and a coupler 30 to which the plurality of connection units 34 is coupled.

Multi-direction Deployable Antenna
20230044114 · 2023-02-09 ·

An antenna system for space applications provides a membrane antenna with one or more flexible membranes. An antenna enclosure stores the membrane antenna during stowage. One or more first deployable support structures extend along a first axis from the antenna enclosure during deployment, at least a first point of the membrane antenna being operably anchored to a point on the first deployable support structures. Deployment mechanisms are operably anchored at a junction with the first deployable support structures. The deployment mechanisms extend one or more second deployable support structures along a second axis from the first deployable support structures during deployment. At least a second point of the membrane antenna is operably anchored to a point on the second deployable support structures. Extension of the first deployable support structures and second deployable support structures unfurls the membrane antenna along both axes to overlap the junction.

DUAL-POLARIZATION ANTENNA

Dual-polarized antenna, including several antenna elements arranged in cell units. Each cell unit includes four antenna elements and two 1-to-4 junctions, a first of the two junctions being associated with a first polarization and a second of the two junctions being associated with a second polarization. The antenna also includes an array of dividers/combiners. The four antenna elements of each cell unit are superposed and several cell units are juxtaposed. Each cell unit includes two antenna elements and two other antenna elements which are offset.

Interleaved phased array antennas
11575204 · 2023-02-07 · ·

Technologies directed to interleaved phased array antennas are described. One apparatus includes a support structure, a first phased array antenna, and a second phased array antenna. The first array antenna includes a first set of antenna elements disposed on a surface of the support structure. The first set of antenna elements are located within a perimeter of a first ellipse. The second antenna includes a second set of antenna elements. The second set of antenna elements are located within a perimeter of a second ellipse. The second ellipse partially overlaps the first ellipse. The majority of the second set of antenna elements are located outside the perimeter of the first ellipse. A majority of the second set of antenna are located in the second ellipse in the area not overlapped by the first ellipse.

Apparatuses for reducing air condensation in components of satcom antenna subsystem

Some embodiments of the present disclosure are directed to an antenna system for an airplane. The antenna system including an antenna system enclosure and a desiccant enclosure within the antenna system enclosure and having desiccant material positioned between an outside air pipe and an inside air pipe, the inside air pipe extending from the desiccant enclosure to open to an interior air volume of at least one component of the antenna system within the antenna system enclosure, the outside air pipe extending from the desiccant enclosure to ambient air outside the antenna system enclosure, and the desiccant material is configured to absorb moisture in the ambient air flowing from the outside air pipe to the inside air pipe through the desiccant enclosure while air pressure is being equalized from outside to inside the antenna system enclosure.

Antenna module grounding for phased array antennas
11705627 · 2023-07-18 · ·

Technologies directed to a radio frequency (RF) structure that provides an electrically insulating gap between a ground plane of a circuit board and a chassis at direct current (DC) and an electrical connection between the ground plane and the chassis at RF frequencies. One RF structure includes a first conductor electrically coupled to the ground plane and a second conductor electrically coupled to the chassis. A physical arrangement of a portion of the first conductor and a portion of the second conductor causes the RF structure to provide an electrically insulating gap between the ground plane and the chassis at DC and an electrical connection between the ground plane and the chassis at RF frequencies.

Surface error reduction for a continuous antenna reflector

The disclosed method may include (1) determining a current physical state regarding an antenna assembly that includes (a) a sub-reflector that receives a wireless signal and reflects the wireless signal to a feed structure for processing, (b) a continuous antenna reflector that receives the wireless signal at a reflecting surface that reflects the wireless signal to the sub-reflector, where the current physical state is indicative of a current surface error over the reflecting surface relative to the sub-reflector, and (c) a backing structure coupled to a back surface of the continuous antenna reflector opposite the reflecting surface and having a plurality of actuators distributed over, and coupled to, the back surface, (2) operating each of the plurality actuators in a manner that reduces the current surface error based on the current physical state. Various other methods and systems are also disclosed.

IMAGING ARRAY FED REFLECTOR

An imaging array fed reflector for a spacecraft is included in a spacecraft payload subsystem. The payload subsystem includes a multi-beam antenna including a reflector, a plurality of amplifiers, and a plurality of radiating feed elements, the feed elements configured as a phased array, illuminating the reflector, operable at a frequency having a characteristic wavelength (λ), and configured to produce, in a far field at the reflector, a set of contiguous abutting beams. The amplifiers are disposed proximate to the plurality of radiating feed elements. Each radiating feed element has a respective coupling with at least one respective amplifier of the plurality of amplifiers. Each radiating feed element, together with the at least one respective amplifier, is disposed in a closely packed triangular lattice such that separation between adjacent radiating feed elements is not greater than 1.5λ.

CHANNEL RECONFIGURABLE MILLIMETER-WAVE RADIO FREQUENCY SYSTEM BY FREQUENCY-AGILE TRANSCEIVERS AND DUAL ANTENNA APERTURES
20180013193 · 2018-01-11 ·

A mobile platform includes an antenna adapted to simultaneously transmit on a first channel and receive on a second channel, and to dynamically switch communication channels as needed. For example, as the mobile platform changes position, orientation, etc., the configuration of the antenna may be updated to transmit on the second channel and receive on the first channel. Accordingly, despite changes in position or orientation, the mobile platform may maintain communication with other mobile platforms, ground controllers, user equipment, etc.